Package org.orekit.propagation.conversion

Interface PropagatorConverter

All Known Implementing Classes:

AbstractPropagatorConverter, FiniteDifferencePropagatorConverter, JacobianPropagatorConverter

public interface PropagatorConverter

This interface is the top-level abstraction for propagators conversions.

It provides a way to convert a given propagator or a set of SpacecraftState into a wanted propagator that minimize the mean square error over a time span.

Since:

6.0

Author:

Pascal Parraud

Method Summary

Modifier and Type	Method	Description
Propagator	convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters)	Find the propagator that minimize the mean square error for a sample of states.
Propagator	convert(List<SpacecraftState> states, boolean positionOnly, List<String> freeParameters)	Find the propagator that minimize the mean square error for a sample of states.
Propagator	convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters)	Convert a propagator into another one.
Propagator	convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters)	Convert a propagator into another one.

Method Detail

convert

Propagator convert(Propagator source,
                   double timeSpan,
                   int nbPoints,
                   List<String> freeParameters)

Convert a propagator into another one.

Parameters:

source - propagator to convert

timeSpan - time span considered for conversion

nbPoints - number of points for sampling over the time span

freeParameters - names of the free parameters

Returns:

adapted propagator

convert

Propagator convert(Propagator source,
                   double timeSpan,
                   int nbPoints,
                   String... freeParameters)

Convert a propagator into another one.

Parameters:

source - propagator to convert

timeSpan - time span considered for conversion

nbPoints - number of points for sampling over the time span

freeParameters - names of the free parameters

Returns:

adapted propagator

convert

Propagator convert(List<SpacecraftState> states,
                   boolean positionOnly,
                   List<String> freeParameters)

Find the propagator that minimize the mean square error for a sample of states.

Parameters:

states - spacecraft states sample to fit

positionOnly - if true, consider only position data otherwise both position and velocity are used

freeParameters - names of the free parameters

Returns:

adapted propagator

convert

Propagator convert(List<SpacecraftState> states,
                   boolean positionOnly,
                   String... freeParameters)

Find the propagator that minimize the mean square error for a sample of states.

Parameters:

states - spacecraft states sample to fit

positionOnly - if true, consider only position data otherwise both position and velocity are used

freeParameters - names of the free parameters

Returns:

adapted propagator